|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:application
|
deep space missions
|
|
gptkbp:cargo_capacity
|
6,000 kg
|
|
gptkbp:cargo_resupply_missions
|
ISS resupply missions
|
|
gptkbp:cargo_types
|
gptkb:ARM
varied by mission
food, water, equipment
|
|
gptkbp:challenges
|
reliability and safety
|
|
gptkbp:collaboration
|
gptkb:NASA
ESA, JAXA, NASA
ESA, NASA, Roscosmos
|
|
gptkbp:communication_system
|
S-band and Ku-band
|
|
gptkbp:control_system
|
autonomous and manual
autonomous docking system
|
|
gptkbp:cooling_system
|
active and passive
|
|
gptkbp:crew
|
no
|
|
gptkbp:crew_capacity
|
gptkb:none
|
|
gptkbp:debut
|
9 missions from 2008 to 2020
|
|
gptkbp:decommissioned
|
gptkb:2020
|
|
gptkbp:design
|
3 years
yes
|
|
gptkbp:designed_by
|
gptkb:JAXA
|
|
gptkbp:developed_by
|
gptkb:Japan_Aerospace_Exploration_Agency
|
|
gptkbp:development
|
gptkb:2000
|
|
gptkbp:development_cost
|
approximately $300 million
|
|
gptkbp:diameter
|
4.4 m
|
|
gptkbp:dimensions
|
10.5 m length
|
|
gptkbp:docking_system
|
gptkb:International_Docking_System_Standard
|
|
gptkbp:durability
|
no
|
|
gptkbp:electrification
|
4.5 k W
|
|
gptkbp:first_flight
|
May 2020
February 2011
September 10, 2008
|
|
gptkbp:flight_style
|
gptkb:9
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-II Transfer Vehicle
|
|
gptkbp:launch_date
|
approximately once a year
|
|
gptkbp:launch_mass
|
16,500 kg
|
|
gptkbp:launch_price
|
approximately $30 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Team_Rocket
gptkb:H-II_rocket
|
|
gptkbp:launch_window
|
varies by mission
varied by ISS schedule
|
|
gptkbp:legacy
|
paved the way for HTV-X
|
|
gptkbp:length
|
9.8 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mass
|
16,500 kg
|
|
gptkbp:mission
|
gptkb:Tsukuba_Space_Center
gptkb:HTV-9
|
|
gptkbp:mission_duration
|
up to 30 days
approximately 30 days
|
|
gptkbp:operates_in
|
gptkb:2020
|
|
gptkbp:operational_period
|
2008 to 2020
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
gptkb:JAXA
|
|
gptkbp:orbit_type
|
low Earth orbit
|
|
gptkbp:orbital_altitude
|
400 km
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:payload_capacity
|
pressurized and unpressurized cargo
automated and manual
to ISS
pressurized and unpressurized
before launch
done at Tanegashima Space Center
|
|
gptkbp:post_mission_disposal
|
burn up in atmosphere
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:pressurized_module_volume
|
14 m³
|
|
gptkbp:primary_function
|
transport supplies
|
|
gptkbp:production_years
|
gptkb:2008
|
|
gptkbp:purpose
|
cargo transport
cargo resupply to the International Space Station
|
|
gptkbp:recovery_method
|
not applicable
|
|
gptkbp:replaced_by
|
gptkb:HTV-X
|
|
gptkbp:safety_features
|
redundant systems
multiple redundancy systems
|
|
gptkbp:service
|
gptkb:HTV_service_module
|
|
gptkbp:signage
|
yes
|
|
gptkbp:speed
|
yes
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:successor
|
gptkb:HTV-X_program
gptkb:HTV-X
|
|
gptkbp:sustainability
|
2
designed for multiple missions
|
|
gptkbp:transportation
|
orbital transportation
|
|
gptkbp:unpressurized_module_volume
|
10 m³
5 m³
|
|
gptkbp:used_for
|
cargo resupply to the International Space Station
|
|
gptkbp:was_a_demonstration_of
|
new technologies for future missions
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:bfsLayer
|
4
|